期刊文献+

基于桥联模型的高可靠计算机设计

Design of High Reliability Computer Based on Bridging Model
原文传递
导出
摘要 机载计算机的任务可靠性对飞机飞行安全至关重要,而提高任务可靠性的一个有效途径就是进行余度设计。文章从研究两种常用的双余度容错模型出发,将桥联模型应用于机载计算机的双余度设计。通过对工作模型的故障容错机制的分析,证明该双余度设计可有效提高机载计算机的任务可靠性,具备一定的工程实用价值。 The mission reliability of utility management computer is critical and essential to aircraft flight safety, and an effective way to improve the mission reliability is to carry out dual redundancy design. Starting from the study of two commonly used reliability models, this paper uses the bridging model in dual-redundant design of utility management computer. The fault-tolerant mechanism analysis of bridging model proves that the dual- redundant design can effectively improve the mission reliability of utility management computer, and has a certain practical value.
出处 《电子技术(上海)》 2012年第7期71-72,70,共3页 Electronic Technology
基金 航空基金项目
关键词 高可靠计算机 任务可靠性 桥联模型 high reliability computer mission reliability bridging model
  • 相关文献

参考文献5

二级参考文献9

  • 1[1]Hermann Kopetz. Real-time systems: design principles for distributed embedded applications. Kluwer,Dordrecht, The Netherlands: The Kluwer International Series in Engineering and Computer Science, 1997. 1 ~14.
  • 2[2]Kenneth Hoyme, Kevin Driscoll. SAFEbus[TM]. IEEE Aerospace and Electronic Systems Magazine, 1993, 8(3):34~39.
  • 3[3]Hermann Kopetz, Günter Grünsteidl. TTP-a protocol for fault-tolerant real-time systems. IEEE Computer,1994,27(1) :14~23.
  • 4[4]Paul S. Miner, Mahyar Malekpour, Wilfredo TorresPomales. Conceptual design of a reliable optical bus (ROBUS). 21st AIAA/IEEE Digital Avionics Systems Conference, Irvine, CA, October 2002.
  • 5[5]Joef Berwanger, et al. FlexRay-the communication system for advanced automotive control systems. SAE 2001 World Congress ,Detroit ,MI ,April 2001.
  • 6[6]Time-Triggered Technology TTTech Computertechnik AG. Time-triggered protocol TTP/C: high-level specification document. Vienna, Austria, July 2002,Specification Edition 1.0.0,Document Number D-032-S-10-028.
  • 7Egoron I N, Kretinin G V, Leshchenko I A. Optimal design and control of gas-turbine engine components: a multicriteria approach[ J ]. Aircraft Engineering and Aerospace Technology, 1997,69(6): 518 - 526
  • 8Proos K A,Steven G P,Querin O M, Xie Y M. Multicriterion evolutionary structural optimization using the weighting and the global criterion methods [ J ]. AIAA Journal, 2001,39(10) :2006 - 2012.
  • 9Engin A,Fred M, Michel G. Cost and safety optimization of structural design specifications [ J ]. Reliability Engineering and System Safety, 2001, 73:205- 212.

共引文献12

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部